View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 57448U 26145.45191635 +.00000000 +00000-0 +13848-6 0 00003
2 57448 43.0028 189.5654 0001815 277.1170 82.9476 15.27568960 00
| Epoch (UTC): | 25 May 2026 10:50:45 |
| Eccentricity: | 0.0001815 |
| inclination: | 43.0028° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 189.5654° |
| argument of perigee: | 277.1170° |
| revolutions per day: | 15.27568960 |
| mean anomaly at epoch: | 82.9476° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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